JP2000006893A - 複合材翼構造 - Google Patents

複合材翼構造

Info

Publication number
JP2000006893A
JP2000006893A JP10176093A JP17609398A JP2000006893A JP 2000006893 A JP2000006893 A JP 2000006893A JP 10176093 A JP10176093 A JP 10176093A JP 17609398 A JP17609398 A JP 17609398A JP 2000006893 A JP2000006893 A JP 2000006893A
Authority
JP
Japan
Prior art keywords
girder
composite
composite material
wing
integrally formed
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP10176093A
Other languages
English (en)
Japanese (ja)
Inventor
Kazuaki Amaoka
和昭 天岡
Hideyuki Sano
英之 佐野
Naoya Takizawa
尚哉 滝沢
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Subaru Corp
Original Assignee
Fuji Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Fuji Heavy Industries Ltd filed Critical Fuji Heavy Industries Ltd
Priority to JP10176093A priority Critical patent/JP2000006893A/ja
Priority to EP99112046A priority patent/EP0967147B1/fr
Priority to DE69911507T priority patent/DE69911507T2/de
Priority to US09/338,551 priority patent/US6237873B1/en
Publication of JP2000006893A publication Critical patent/JP2000006893A/ja
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
JP10176093A 1998-06-23 1998-06-23 複合材翼構造 Pending JP2000006893A (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP10176093A JP2000006893A (ja) 1998-06-23 1998-06-23 複合材翼構造
EP99112046A EP0967147B1 (fr) 1998-06-23 1999-06-22 Structure d'aile en matériau composite
DE69911507T DE69911507T2 (de) 1998-06-23 1999-06-22 Flügelstruktur aus Faserverbundstoff
US09/338,551 US6237873B1 (en) 1998-06-23 1999-06-23 Composite material wing structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10176093A JP2000006893A (ja) 1998-06-23 1998-06-23 複合材翼構造

Publications (1)

Publication Number Publication Date
JP2000006893A true JP2000006893A (ja) 2000-01-11

Family

ID=16007588

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10176093A Pending JP2000006893A (ja) 1998-06-23 1998-06-23 複合材翼構造

Country Status (4)

Country Link
US (1) US6237873B1 (fr)
EP (1) EP0967147B1 (fr)
JP (1) JP2000006893A (fr)
DE (1) DE69911507T2 (fr)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002302097A (ja) * 2001-04-05 2002-10-15 Fuji Heavy Ind Ltd 複合材翼およびその製造方法
JP2003072691A (ja) * 2001-09-03 2003-03-12 Fuji Heavy Ind Ltd 複合材翼の製造方法および複合材翼
JP2006512240A (ja) * 2002-06-20 2006-04-13 ロッキー マウンテン コンポジッツ インコーポレイテッド 一体同時硬化複合材翼
JP2007125890A (ja) * 2005-11-01 2007-05-24 Boeing Co:The ツールアセンブリ、航空機の翼、航空機の翼および翼外板の製造方法、ならびに複合積層体を製造するためのシステム
US7681835B2 (en) 1999-11-18 2010-03-23 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
JP2010523397A (ja) * 2007-04-05 2010-07-15 ザ・ボーイング・カンパニー 複合トラス構造のための方法とシステム
JP2011152753A (ja) * 2010-01-28 2011-08-11 Honda Motor Co Ltd 航空機翼構造の成形方法
JP2012523348A (ja) * 2009-04-09 2012-10-04 エアバス オペレーションズ リミテッド 改良型ウイング構造体
JP2013521438A (ja) * 2010-03-10 2013-06-10 ヴォッベン プロパティーズ ゲーエムベーハー 風力エネルギー設備用ロータブレード
WO2013099110A1 (fr) * 2011-12-27 2013-07-04 三菱航空機株式会社 Prise d'air, panneau d'aile et aile principale pour avion
CN103339028A (zh) * 2011-02-04 2013-10-02 三菱重工业株式会社 复合材料构造体及具备该复合材料构造体的航空器主翼
JP2014104975A (ja) * 2012-11-26 2014-06-09 Boeing Co マルチボックス翼スパーおよび外板
JP2015515940A (ja) * 2012-05-02 2015-06-04 イートン リミテッドＥａｔｏｎ Ｌｉｍｉｔｅｄ 航空機燃料タンク不活性システム
US9108718B2 (en) 2009-10-08 2015-08-18 Mitsubishi Heavy Industries, Ltd. Composite-material structure and aircraft main wing and aircraft fuselage provided with the same
JP2015227154A (ja) * 2013-12-20 2015-12-17 エアバス オペレイションズ エスエーエス 主翼ボックスを作製する方法
US9751608B2 (en) 2011-02-04 2017-09-05 Mitsubishi Heavy Industries, Ltd. Composite material structure, and aircraft wing and aircraft fuselage provided therewith

Families Citing this family (63)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6513757B1 (en) * 1999-07-19 2003-02-04 Fuji Jukogyo Kabushiki Kaisha Wing of composite material and method of fabricating the same
ES2197727B1 (es) * 2000-07-27 2005-04-01 Construcciones Aeronauticas, S.A. Borde de ataque de superficies sustentadoras de aeronaves.
US7204951B2 (en) * 2002-07-30 2007-04-17 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
FR2846939A1 (fr) * 2002-11-13 2004-05-14 Soc D Const Aeronautique Auver Procede de fabrication d'une aile d'avion leger
US6811120B1 (en) * 2003-04-15 2004-11-02 Adam Aircraft Industries, Inc. Modular spar tunnel
US7244487B2 (en) * 2003-04-24 2007-07-17 Lockheed Martin Corporation Apparatus, system, and method of joining structural components with a tapered tension bond joint
US20040213953A1 (en) * 2003-04-24 2004-10-28 Lockheed Martin Corporation Apparatus, system, and method of joining structural components with a tapered tension bond joint
ATE441573T1 (de) * 2003-05-09 2009-09-15 Pilatus Flugzeugwerke Ag Flugzeugflügel
AU2003262925A1 (en) * 2003-08-27 2005-04-14 Bell Helicopter Textron Inc. Protective skin for aircraft
US7182293B2 (en) * 2004-04-27 2007-02-27 The Boeing Company Airfoil box and associated method
US7387277B2 (en) * 2004-12-29 2008-06-17 The Boeing Company Aircraft wing composed of composite and metal panels
US8544800B2 (en) * 2005-07-21 2013-10-01 The Boeing Company Integrated wingtip extensions for jet transport aircraft and other types of aircraft
DE102005038851A1 (de) 2005-08-17 2007-03-01 Airbus Deutschland Gmbh Fachwerk-Mittelkasten für einen Flügel
FI118761B (fi) 2006-02-09 2008-03-14 Patria Aerostructures Oy Ilma-aluksen siipi, kiinnitysjärjestely sekä välituki
US7517198B2 (en) * 2006-03-20 2009-04-14 Modular Wind Energy, Inc. Lightweight composite truss wind turbine blade
US7976282B2 (en) 2007-01-26 2011-07-12 General Electric Company Preform spar cap for a wind turbine rotor blade
CN101595300A (zh) * 2007-01-29 2009-12-02 丹麦技术大学 风力涡轮机叶片
WO2008132251A1 (fr) * 2007-04-30 2008-11-06 Airbus España, S.L. Caisson de torsion multi-longerons intégré en matériau composite
ES2346834B1 (es) * 2007-04-30 2011-08-17 Airbus Operations, S.L. Estructura de costilla para cajones de torsion de un ala o de un estabilizador de una aeronave.
US7900876B2 (en) * 2007-08-09 2011-03-08 The Boeing Company Wingtip feathers, including forward swept feathers, and associated aircraft systems and methods
US7828246B2 (en) * 2007-09-14 2010-11-09 Spectrum Aeronautical, Llc Wing with sectioned tubular members
US7871041B2 (en) * 2007-10-17 2011-01-18 Lockheed Martin Corporation System, method, and apparatus for leading edge structures and direct manufacturing thereof
DE102008013365B4 (de) * 2008-03-10 2011-03-17 Airbus Operations Gmbh Querstoßverbindung zwischen zwei Rumpfsektionen
US8128035B2 (en) * 2008-04-15 2012-03-06 The Boeing Company Winglets with recessed surfaces, and associated systems and methods
GB0807515D0 (en) * 2008-04-24 2008-06-04 Blade Dynamics Ltd A wind turbine blade
US8777579B2 (en) * 2008-06-20 2014-07-15 Vestas Wind Systems A/S Method of manufacturing a spar for a wind turbine from elements comprising different materials
US8777578B2 (en) * 2008-06-20 2014-07-15 Vestas Wind Systems A/S Method of manufacturing a spar for a wind turbine from elements having geometrically well-defined joint surface portions
CN201225330Y (zh) * 2008-06-24 2009-04-22 陈清辉 木质吊扇叶片
WO2010053775A1 (fr) * 2008-10-29 2010-05-14 Delta T Corporation Section de profil aérodynamique modulaire multi-pièces et procédé pour la fixation entre des pièces
US20100107513A1 (en) * 2008-11-03 2010-05-06 Buchanan Kenneth K Pre-Cured Edge Seal
US20100116938A1 (en) * 2008-11-13 2010-05-13 Kline William T Method and apparatus for joining composite structural members and structural members made thereby
US8307872B2 (en) 2008-11-13 2012-11-13 The Boeing Company Apparatus for curing a composite structural member
US9669579B2 (en) 2008-11-13 2017-06-06 The Boeing Company Aircraft skin attachment system
CN102308083B (zh) 2008-12-05 2016-04-13 模组风能公司 高效风轮机叶片
ES2372828B1 (es) * 2008-12-17 2012-12-13 Airbus Operations, S.L. Costilla-herraje.
US9500179B2 (en) 2010-05-24 2016-11-22 Vestas Wind Systems A/S Segmented wind turbine blades with truss connection regions, and associated systems and methods
ES2606245T3 (es) * 2012-07-17 2017-03-23 Airbus Operations, S.L. Borde de ataque altamente integrado de una superficie sustentadora de una aeronave
US10118686B2 (en) * 2012-09-27 2018-11-06 The Boeing Company Wing root insert system for an aircraft family
EP2735502B1 (fr) * 2012-11-21 2016-08-24 Airbus Operations S.L. Caisson de torsion optimisé pour aéronef
US9446835B2 (en) 2013-01-16 2016-09-20 Otto Aviation Group Aircraft wing
US8973871B2 (en) 2013-01-26 2015-03-10 The Boeing Company Box structures for carrying loads and methods of making the same
US9470205B2 (en) 2013-03-13 2016-10-18 Vestas Wind Systems A/S Wind turbine blades with layered, multi-component spars, and associated systems and methods
GB2515044A (en) * 2013-06-12 2014-12-17 Airbus Operations Ltd Aircraft wing arrangement
EP2886449A1 (fr) * 2013-12-23 2015-06-24 Airbus Operations S.L. Bord d'attaque pour surface de sustentation d'un aéronef
US10272619B2 (en) * 2014-05-19 2019-04-30 The Boeing Company Manufacture of a resin infused one-piece composite truss structure
DE102015103021A1 (de) * 2015-03-03 2016-09-08 Ellergon Antriebstechnik Gesellschaft M.B.H. Hydrofoilfinne
EP3095691A1 (fr) * 2015-05-22 2016-11-23 Airbus Operations, S.L. Structure de caisson de torsion multi-poteau
US10724994B2 (en) 2015-12-15 2020-07-28 University Of South Carolina Structural health monitoring method and system
US10207789B2 (en) 2016-08-16 2019-02-19 The Boeing Company Aircraft composite wingbox integration
US10421528B2 (en) 2016-08-16 2019-09-24 The Boeing Company Planked stringers that provide structural support for an aircraft wing
US10609771B2 (en) 2016-08-18 2020-03-31 University Of South Carolina Printable susceptor for use in induction welding
US20180086429A1 (en) * 2016-09-28 2018-03-29 The Boeing Company Airfoil-Shaped Body Having Composite Base Skin with Integral Hat-Shaped Spar
GB2557274A (en) * 2016-12-02 2018-06-20 Airbus Operations Ltd Aerofoil structure components
IT201700122745A1 (it) * 2017-10-27 2019-04-27 Salver S P A Procedimento di assemblaggio di parti di un’ala aeronautica
US10647407B2 (en) 2018-03-30 2020-05-12 The Boeing Company Wing flap with torque member and method for forming thereof
US10759516B2 (en) 2018-03-30 2020-09-01 The Boeing Company Wing flap with torque member and method for forming thereof
US10597141B2 (en) 2018-03-30 2020-03-24 The Boeing Company Wing flap with torque member and method for forming thereof
US11022561B2 (en) 2018-10-08 2021-06-01 University Of South Carolina Integrated and automated video/structural health monitoring system
US11459085B2 (en) * 2019-04-30 2022-10-04 Textron Innovations Inc. Energy attenuation stabilizers and methods
US11046420B2 (en) * 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure
US11352124B2 (en) * 2019-11-01 2022-06-07 The Boeing Company Continuous skin leading edge slats
US11623734B2 (en) 2020-12-02 2023-04-11 The Boeing Company Apparatus, system and method for supporting a wing flap of an aircraft
EP4552816A1 (fr) * 2023-11-07 2025-05-14 Airbus Operations, S.L.U. Procédé de fabrication de lisses en forme de y et lisses en forme de y double en matériau composite

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB303360A (en) * 1927-12-31 1929-11-07 Rohrbach Metall Flugzeugbau Ge Improvements in metal aircraft wings
US5332178A (en) * 1992-06-05 1994-07-26 Williams International Corporation Composite wing and manufacturing process thereof
DE4315600C2 (de) * 1993-05-11 1996-07-25 Daimler Benz Aerospace Airbus Tragstruktur für eine aerodynamische Fläche
DE19528664C2 (de) * 1995-08-04 1997-07-31 Joachim Heyse Tragkörper aus einem Verbundwerkstoff
DE19529476C2 (de) * 1995-08-11 2000-08-10 Deutsch Zentr Luft & Raumfahrt Flügel mit schubsteifen Flügelschalen aus Faserverbundwerkstoffen für Luftfahrzeuge
US5848765A (en) * 1996-06-20 1998-12-15 The Boeing Company Reduced amplitude corrugated web spar

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7681835B2 (en) 1999-11-18 2010-03-23 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
JP2002302097A (ja) * 2001-04-05 2002-10-15 Fuji Heavy Ind Ltd 複合材翼およびその製造方法
JP2003072691A (ja) * 2001-09-03 2003-03-12 Fuji Heavy Ind Ltd 複合材翼の製造方法および複合材翼
JP2006512240A (ja) * 2002-06-20 2006-04-13 ロッキー マウンテン コンポジッツ インコーポレイテッド 一体同時硬化複合材翼
JP2007125890A (ja) * 2005-11-01 2007-05-24 Boeing Co:The ツールアセンブリ、航空機の翼、航空機の翼および翼外板の製造方法、ならびに複合積層体を製造するためのシステム
JP2010523397A (ja) * 2007-04-05 2010-07-15 ザ・ボーイング・カンパニー 複合トラス構造のための方法とシステム
JP2012523348A (ja) * 2009-04-09 2012-10-04 エアバス オペレーションズ リミテッド 改良型ウイング構造体
US9108718B2 (en) 2009-10-08 2015-08-18 Mitsubishi Heavy Industries, Ltd. Composite-material structure and aircraft main wing and aircraft fuselage provided with the same
JP2011152753A (ja) * 2010-01-28 2011-08-11 Honda Motor Co Ltd 航空機翼構造の成形方法
JP2013521438A (ja) * 2010-03-10 2013-06-10 ヴォッベン プロパティーズ ゲーエムベーハー 風力エネルギー設備用ロータブレード
CN103339028A (zh) * 2011-02-04 2013-10-02 三菱重工业株式会社 复合材料构造体及具备该复合材料构造体的航空器主翼
US9027881B2 (en) 2011-02-04 2015-05-12 Mitsubishi Heavy Industries, Ltd. Composite material structure and aircraft wing provided therewith
US9751608B2 (en) 2011-02-04 2017-09-05 Mitsubishi Heavy Industries, Ltd. Composite material structure, and aircraft wing and aircraft fuselage provided therewith
WO2013099110A1 (fr) * 2011-12-27 2013-07-04 三菱航空機株式会社 Prise d'air, panneau d'aile et aile principale pour avion
JP2013133035A (ja) * 2011-12-27 2013-07-08 Mitsubishi Aircraft Corp ベント部材、航空機の主翼
US9926082B2 (en) 2011-12-27 2018-03-27 Mitsubishi Aircraft Corporation Vent member, wing panel, and main wing for aircraft
JP2015515940A (ja) * 2012-05-02 2015-06-04 イートン リミテッドＥａｔｏｎ Ｌｉｍｉｔｅｄ 航空機燃料タンク不活性システム
US10633108B2 (en) 2012-05-02 2020-04-28 Eaton Intelligent Power Limited Aircraft fuel tank inerting system
JP2014104975A (ja) * 2012-11-26 2014-06-09 Boeing Co マルチボックス翼スパーおよび外板
JP2015227154A (ja) * 2013-12-20 2015-12-17 エアバス オペレイションズ エスエーエス 主翼ボックスを作製する方法

Also Published As

Publication number Publication date
DE69911507T2 (de) 2004-06-24
US6237873B1 (en) 2001-05-29
EP0967147A2 (fr) 1999-12-29
EP0967147A3 (fr) 2002-04-24
DE69911507D1 (de) 2003-10-30
EP0967147B1 (fr) 2003-09-24

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